Office of Aviation Services Master UAS Requirements for the DOI

Department of the Interior Master UAS Requirements for the DOI

Office of Aviation Services Version: 1.3

NOTICE:

REQUIREMENTS OUTLINED IN THE ATTACHED ARE USED TO INFORM CURRENT AND FUTURE DOI UAS PROCUREMENTS. ACTUAL PROCUREMENTS ARE DRIVEN BY CURRENT DEPARTMENT/BUREAU PRIORITIES, AVAILABLE FUNDING, AND STAFFING NECESSARY TO SUPPORT THE MANAGEMENT AND EMPLOYMENT OF ACQUIRED .

ONLY OFFICIAL COPY OF THIS DOCUMENT IS THE ELECTRONIC COPY THAT CAN BE FOUND ON THE DOI UAS NEWS AND MEDIA WEBPAGE: https://www.doi.gov/aviation/uas/news

Document: Master UAS Requirements for the DOI 1 Revision: 1.3 Office of Aviation Services Master UAS Requirements for the DOI

TABLE OF CONTENTS

A. PURPOSE ...... 3

B. APPLICABILITY ...... 3

C. IMPACTED LINE ITEMS ...... 3

D. DOCUMENT APPROVING AUTHORITY AND CUSTODIAN ...... 3

E. DOCUMENT REVIEW AND REVISION HISTORY ...... 3

F. RELATED METHODOLOGIES AND REFERENCES ...... 3

G. INPUTS AND OUTPUTS ...... 4

H. PROCESS NARRATIVE ...... 4

I. MASTER SPECIFICATION……………………………………………………………………………5

Document: Master UAS Requirements for the DOI 2 Revision: 1.3

Office of Aviation Services Master UAS Requirements for the DOI

A. BACKGROUND & PURPOSE

BACKGROUND: Solid, mission-based requirements are core to the success of any professionally managed aviation program. DOI began its UAS requirements determination process when the current program was initiated in 2006. Later, leveraging hundreds of excess DOD small UAS, OAS and Interior bureaus conducted hundreds of operational test and evaluation flights that were used to inform the initial development of a set of master UAS requirements. In 2014, over 300 bureau and OAS subject matter experts came together to draft the initial requirements document. The requirements document guides Interior’s market research and subsequent acquisitions for UAS and/or contracted services. Updates to UAS requirements are identified and proposed through formal feedback from field users channeled through appropriate DOI aviation management (e.g. bureau national aviation managers) and established advisory groups. Revisions are issued when the Master UAS Requirements are updated.

PURPOSE: To provide for dissemination and version control of DOI UAS Master Requirements for the DOI.

B. APPLICABILITY

This process is applicable to Master UAS Requirements for the DOI.

C . IMPACTED LINE ITEMS

This process has no impact on Department of the Interior Financial Statements prepared by the IBC.

D. DOCUMENT APPROVING AUTHORITY AND CUSTODIAN

Document Number: Master UAS Requirements Approved by: B. Koeckeritz Document Revision: 1.3 Title: OAS UAS DC Next Review Due: 3/15/2019 Date Approved: 3/15/19 Document Custodian: OAS UAS Effective Date: 3/15/19

E. DOCUMENT REVIEW AND REVISION HISTORY

Date Document Document Revision Description Document Author Revision Revision 1 Initial Publication Ramaekers

04/11/2018 1.1 Add VTOL Stroud

10/08/18 1.2 Add CWN ISR Stroud

Add #9 Training Multi Rotor / Remove “Up to 2 hrs #1 03/15/19 1.3 Stroud CWN”

F . RELATED METHODOLOGIES AND REFERENCES

OAS Quality Manual All core processes

Document: Master UAS Requirements for the DOI 3 Revision: 1.3 Office of Aviation Services Master UAS Requirements for the DOI

G. INPUTS AND OUTPUTS

The principle input(s) into this process are: 1. Changes, edits or additions to the Master UAS Requirements The principle output(s) from this process are: 1. Updated Master UAS Requirements document

H. PROCESS NARRATIVE

1. New and updated UAS requirements are identified and proposed through formal feedback from field users channeled through appropriate DOI aviation management (e.g. bureau national aviation managers) and established advisory groups.

2. OAS UAS determines whether the proposed requirement is one already covered by current requirements and equipment. OAS also conducts an assessment of whether the requirement can be met within the current legal, regulatory, and policy framework for safely and responsibly operating UAS.

3. If the proposed new/updated requirement is determined to be redundant or outside the bounds of the current legal, regulatory, and policy framework for safely and responsibly operating UAS, the Master UAS Requirements is unchanged. If the proposed new/updated requirement is determined to be valid, the Master UAS Requirements is edited.

4. Process ends.

Document: Master UAS Requirements for the DOI 4 Revision: 1.3 U.S. Department of the Interior Master UAS Requirements V1.3 - March 15, 2019 #1 CALL WHEN NEEDED (CWN) ISR

Flight Performance

Item Minimum Specification Target Specification

Fixed wing, hand launch/assisted launch or VTOL, Aircraft Type runway independent, 55 pounds or less.

DOI Aircraft and Flight Crew Authorization (carded AC and crew) Vendor may be required to Airworthiness complete DOI/NASA airworthiness review process at their expense

Takeoff/Recovery Maximum area of 300’x300’ Maximum area of 200’x200’ Area

5000' AGL @ 3000' MSL @ 32° C Service Ceiling 5000' AGL @ 8000' MSL @ 30° C

2 hours (with fuel/batteries on site to fly for 12 Flight Duration Up to 14 hours hours)

Wind Limit /: 20 knots. Takeoff/landing: 30 knots

Wind Limit Operate in sustained winds of 25 knots Operate in sustained winds of 35 knots

Operational Day and night capable window

Operational temperature of 32-100 degrees Operational temperature of 0-115 degrees Temperature Fahrenheit Fahrenheit

Command and Control

Item Minimum Specification Target Specification

Range C2 range of >5nm C2 range of >15nm

Secure digital data link with FIPS Uplink Frequency compliant encryption

Downlink Secure digital data link with FIPS Frequency compliant encryption

Loss of Link (LOL) capability: return Selectable LOL: Return to launch, land now, route Lost Link to launch or land now. retrace, programmable point.

Ability to program restricted areas of Ability to program a flight plan based on a GIS Flight Planning operations (geo-fence) produced polygon (shape file)

Ability to loiter at an assigned altitude Flight profile with <200’ deviation

5 V1.3 - March 15, 2019 #1 CWN ISR

Transponder Mode C programmable Mode C/S programmable

TCAS TCAS unit at ground station

Programmable based on altimeter Altimeter setting (inHG)

Location displayed on GCS in UAS Location latitude and longitude in degrees, Display decimal minutes (DDD MM.MM) format

UAS Altitude Altitude displayed on GCS in feet Display above mean sea level (MSL)

Programmable VHF AM and FM at Programmable VHF AM and FM mounted in Radios ground station (FCC compliant) the UAS

Compliant with DOI, DOA, FAA Operations policy (COA, ECOA, MOA, etc.)

Payload

Item Minimum Specification Target Specification

Gimbal - General Gyro stabilized dual sensor Customizable multi-sensor gimbal (radiometric, gas, (EO/IR) smoke, etc.)

Gimbal – EO video Real-time HD (720p) video Real-time HD (1080p) video

Real-time (mid-long wave) IR Real-time mid-wave (1.5-5.6um) IR video (TASE 400 Gimbal – IR video video (1.5-10 um LRS or similar)

Gimbal EO and IR Capture still images in EO Images and IR High resolution EO/IR zoom (30-50x)

Map a fire perimeter with Transmit data to Federal Data Specialist laptop to Gimbal - Mapping the target cursor or other process with ERSI Full Motion Video (FMV) means Object Tracking Ability to lock gimbal on Ability to lock gimbal on moving POI stationary POI

Mapping - Other DSLR payload for ortho-image mapping

6 V1.3 - March 15, 2019 #1 CWN ISR

Data Standards

Item Minimum Specification Target Specification

Telemetry Provide flight telemetry data upon request.

Capture/transmit ESRI compliant video Provide extractable GIS metadata (MSBI Video to be viewed/edited with the ERSI Full compliant) for both EO and IR Motion Video (FMV) extension

Capture incremental GPS points around a Fire Perimeter fire perimeter and export them as a KML or Map and share fire perimeter in real-time Data SHP file. Tolerance for GPS points is 30’.

Capture geotagged still images/videos as Points of Interest directed. Geotagging format is DDD Share geotagged images in real-time MM.MM. GPS tolerance is 30’

Vendor will deliver/destroy data in Data storage compliance with federal standards.

Ground Terminal

Item Minimum Specification Target Specification

50” monitor displaying live EO/IR Transmit video feed to a remote terminal at the incident gimbal feed at ground station. command post (ICP) or designated location using Live Video Feed Display will be split screen with wave/mesh/ad-hoc/MIMO networking or other contextual map (fire perimeter) technology and camera view

Time Requirements

Item Minimum Specification Target Specification

Vendor will be on site and Vendor will be on site and operational within 24 hours Mobilization operational within 72 hours, or mutually agreed upon time of of dispatch dispatch GIS (point, line, polygon) data will be delivered to Telemetry data will be provided Data Delivery incident personal within 1 hour of request Compliant within 4 hours of request GIS and video data will be delivered to incident personal within 1 hour of request

7 V1.3 - March 15, 2019 #1 CWN ISR

Launch (once on site and One hour after request 15 minutes after request available)

Gimbal will be tasked within 30 Gimbal Tasking Gimbal will be tasked within 5 minutes of request minutes of request

Miscellaneous

Item Minimum Specification Target Specification

Invoicing Vendor will utilize existing federal invoicing systems

Procedural Vendor crews will attend one week of BLM fire procedures Training training. This training will include flight exercises with vendor UAS and sensors.

Vendor crews will attend basic wildland firefighter and fire Fireline Training shelter training (S-130/190)

Vendor crews will have required fireline personnel protective equipment (PPE) on site. Required PPE is Fireline Equipment listed in the Interagency Standards for Fire and Fire Aviation Operations

Camping/Logistics Crews will be prepared to operate in remote areas and be Equipment self-sufficient for three days.

8 V1.3 - March 15, 2019 #2 Fixed VTOL

Flight Performance Minimum UAS Requirement Target UAS Requirement Platform weight under 25 lbs. Platform weight under 10 lbs. Flight duration of 90 minutes with maximum payload, standard Flight duration of 30 minutes with max payload, standard day. day. Service ceiling 10,500 feet density altitude. Service ceiling 17,999 feet density altitude. Maximum sustained wind speed capability of 15 knots. Maximum sustained wind speed capability of 35 knots. Minimum launch area requirement of 50 feet by 50 feet. Minimum launch area requirement of 20 feet by 20 feet. Minimum recovery area requirement of 50 feet by 50 feet. Minimum recovery area requirement of 20 feet by 20 feet. Vertical Take Off and Vertical Landing N/A Vertical Take Off and Vertical Landing from a boat N/A Operating temperature range of negative 40–130 degrees Operating temperature range of 10–110 degrees Fahrenheit. Fahrenheit. Environmental criteria of day/night time aircraft lighting N/A (FAR part 91 section 209) N/A Environmental criteria of being water proof.

Command and Control Minimum UAS Requirement Target UAS Requirement Communication range (RX/TX) C2 of 2 Nautical Miles. Communication range (RX/TX) C2 of 3 Nautical Miles. N/A Real Time Kinematic (RTK) GPS Transmit video up to 2 Nautical Miles Transmit video up to 3 Nautical Miles Electric N/A Uplink control frequency that is a secure digital data link at 2.4 GHz and or 5.8 GHz ISM Bands and or 900mhz, w/FIPS N/A compliant WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Downlink frequency that is a secure digital data link at 2.4 GHz and or 5.8 GHz ISM Bands and or 900mhz, N/A w/FIPS compliant WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Programmable Loss of Link (LOL) capability: return to Loss of Link (LOL): route retrace, land at a specified location. launch and land now. Ground Control Station (GCS) provided and capable of N/A importing shapefiles. Aircraft can navigate by waypoints while making altitude Aircraft has the ability to navigate by waypoints. changes allowing terrain following.

Payload Minimum UAS Requirement Target UAS Requirement Configurable payload weight of 1.5 lbs. Configurable payload weight of 5 lbs. Real time video EO forward looking (independent of payload) to provide UAS pilot with situational awareness during daytime, N/A nighttime and low light missions with ability to record video stream. Aircraft is equipped with modular payload design with plug N/A and play swappable COTS cameras or sensors. Gimbal EO/IR payload. Gimbal EO/IR payload with on-board storage. Gimbal IR payload. Gimbal IR payload with on-board recording. DSLR camera mounted to gimbal stabilized mount (option to be DSLR camera fixed Nadir mount. fixed at the nadir position). Provide technical specifications for payload interface. N/A

9 V1.3 - March 15, 2019 #2 Fixed VTOL

Aircraft autopilot system has the ability to GPS trigger the payload based on GPS location or GPS/IMU distance for appropriate stereo coverage and image overlap at the desired N/A stock payload configuration for photogrammetric stereo imaging. Capable to integrate DGPS/RTK into imagery metadata for high N/A precision mapping missions. Provide MISB (motion imagery standards board) MUXE Video N/A for HD quality or better. The Aircraft IMU telemetry should be embedded into the video metadata.

Miscellaneous Specifications Minimum UAS Requirement Target UAS Requirement A service manual provided. N/A Mission planning software must be able to program multiple GPS waypoints with the ability to modify flight plans while in N/A flight. Aircraft, GCS and battery charging system are included with Aircraft, GCS and battery charging system are included with protective shipping/carrying hard cases. Cases must be protective shipping/carrying/back-packable cases. Cases must allowed as checked baggage on commercial airlines and be allowed as checked baggage and on commercial airlines and deliverable by shipping services. deliverable by shipping services. Ability to decline and lock out any device information sharing including telemetry through aircraft, software or applications N/A preventing any automated uploads or downloads. Optional Customer Support Customer Support VTOL FW Fixed Wing Vertical Take-off and Landing (VTOL) with RTK Fixed Wing VTOL without RTK and Base Station Payloads: Sony a6000 Sony a7R SLANTRANGE 3p MicaSense RedEdge Gimbaled FLIR Vue Pro R 640 (19mm,30Hz) Colibri EO/IR Gimbal Richo GR II Ground Control Station Computer: Dell (Rugged with i7 processor and 64 GB Ram)

10 V1.3 - March 15, 2019 #3 Medium Fixed

Flight Performance Target UAS Requirements (In addition to minimum Minimum UAS Requirement requirements) Platform weight under 25 lbs. Platform weight under 10 lbs. Flight duration of 90 minutes with maximum payload, Flight duration of 60 minutes with max payload, standard day. standard day. Service ceiling 12,500 feet density altitude. Service ceiling 15,999 feet density altitude. Maximum sustained wind speed capability of 25 knots. Maximum sustained wind speed capability of 35 knots. Minimum launch area requirement of 100 feet by 100 Minimum launch area requirement of 300 feet by 300 feet. feet. Minimum recovery area requirement of 100 feet by 100 Minimum recovery area requirement of 300 feet by 300 feet. feet. Assisted launch or hand launched Assisted launch method. Recovery by belly landing or parachute or deep stall or net. Water recovery. Noise level of 50 dB at 300 feet (AGL) at full power. Noise level of 50 dB at 100 feet (AGL) at full power. Operating temperature range of negative 40–110 degrees Operating temperature range of 10–110 degrees Fahrenheit. Fahrenheit. Environmental criteria of day/night time aircraft lighting (FAR part Environmental criteria of being water proof. 91 section 209), water resistant (light rain, snow, mist).

Command and Control Target UAS Requirements (In addition to minimum Minimum UAS Requirement requirements) Communication range (RX/TX) C2 of 2 Nautical Miles. Communication range (RX/TX) C2 of 5 Nautical Miles. Transmit video up to 2 Nautical Miles. Transmit video up to 5 Nautical Miles. Electric, gas, turbine power supply, Fuel cell Power supply non-aviation fuel. Uplink control frequency that is a secure digital data link at 900 N/A MHz ISM Band, w/ 256 bit encryption. Downlink frequency that is a secure digital data link at 2.4 GHz and N/A or 5.8 GHz ISM Bands and or 900mhz, w/ 256 bit encryption. Programmable Loss of Link (LOL) capability: return to launch and Loss of Link (LOL): route retrace, land at a specified land now. location. Aircraft is designed to be interoperable with a medium N/A fixed wing/rotor aircraft, includes; common battery, common GCS and common payloads. Ground Control Station (GCS) provided and capable of controlling N/A the aircraft offered. GCS is open source with the ability to be customized to GCS ability to be customized to operate numerous fixed wing and operate numerous fixed wing and rotor wing platforms rotor wing platforms with aircraft direct control authority. with aircraft direct control authority. Flight Operations are geofence restricting operations to G Direct pilot control authority, semi-autonomous flight modes. airspace with self-limiting capabilities. Flight crew required a maximum of 1, not including Flight crew required a maximum of 2, not including observer. observer. Flight planning software must be able to program multiple GPS Aircraft has the ability to navigate by waypoints at a fixed waypoints with in flight line modifiable options. elevation above the ground based on the terrain. Ability to record sensor data on-board the aircraft. N/A

Payload Target UAS Requirements (In addition to minimum Minimum UAS Requirement requirements) Configurable payload weight of 1.5 lbs. Configurable payload weight of 5 lbs. 11 V1.3 - March 15, 2019 #3 Medium Fixed

Real time video EO forward looking (independent of payload) to provide UAS pilot with situational awareness during daytime, Real time video HD EO/IR gimbal payload. nighttime and low light missions with ability to record video stream (IR night vision capability (NVG). Aircraft is equipped with modular payload design with easily Interface with aircraft IMU/GPS and autopilot (Digital swappable COTS cameras or sensors. interface solution). HD EO/Thermal IR payload with fixed or gimbal mount for DSLR, RTK capability. mirrorless interchangeable lens camera. N/A Gimbal HD EO and Thermal IR video. DSLR camera mounted to gimbal stabilized mount N/A (option to be fixed at the nadir position). Payload interface must provide 5 VDC; 12-14.5 VDC, Provide technical specifications for payload interface. Serial, USB, and Ethernet connections. Aircraft autopilot system has the ability to GPS trigger the payload based on GPS location or GPS/IMU distance for appropriate stereo N/A coverage and image overlap at the desired stock payload configuration for photogrammetric stereo imaging. Capable to integrate DGPS/RTK into imagery metadata N/A for high precision mapping missions. Provide MISB (motion imagery standards board) MUXE N/A Video for HD quality or better. The Aircraft IMU telemetry should be embedded into the video metadata.

12 V1.3 - March 15, 2019 #4 Micro Fixed

Flight Performance

Minimum UAS Requirement Target UAS Requirements

Platform weight under 10 lbs. Platform weight under 8 lbs. Flight duration of 4 hours with maximum payload, Flight duration of 2 hours with max payload, standard day. standard day. Service ceiling 10,500 feet density altitude. Service ceiling 15,999 feet density altitude. Maximum sustained wind speed capability of 25 knots. Maximum sustained wind speed capability of 35 knots. Minimum launch area requirement of 100 feet by 100 Minimum launch area requirement of 300 feet by 300 feet. feet. Minimum recovery area requirement of 300 feet by 300 Minimum recovery area requirement of 300 feet by 300 feet. feet. Assisted launch or hand launched or VTOL. Assisted launch method. Recovery by belly landing. Water recovery. Noise level of 60 dB at 100 feet (AGL) at full power. Noise level of 50 dB at 100 feet (AGL) at full power. Operating temperature range of negative 40–110 degrees Operating temperature range of 10–110 degrees Fahrenheit. Fahrenheit. Environmental criteria of day/night time aircraft lighting (FAR Environmental criteria of being water proof. part 91 section 209), water resistant (light rain, snow, mist). Surge Flight Speed 45 knots. Surge Flight Speed 50 knots.

Command and Control

Minimum UAS Requirement Target UAS Requirements Communication range (RX/TX) C2 of 2 Nautical Miles. Communication range (RX/TX) C2 of 5 Nautical Miles. Transmit video up to 2 Nautical Miles. Transmit video up to 5 Nautical Miles. Electric power supply. N/A Uplink control frequency that is a secure digital data link at N/A 900 MHz ISM Band, w/ 256 bit encryption. Downlink frequency that is a secure digital data link at 2.4 GHz and or 5.8 GHz ISM Bands and or 900mhz, w/ 256 bit N/A encryption Programmable Loss of Link (LOL) capability: return to launch Loss of Link (LOL): route retrace, land at a specified and land now. location. Aircraft is designed to be interoperable with a medium N/A fixed wing/rotor aircraft, includes; common battery, common GCS and common payloads. Ground Control Station (GCS) provided and capable of N/A controlling the aircraft offered. GCS is open source with the ability to be customized to GCS ability to be customized to operate numerous fixed wing operate numerous fixed wing and rotor wing platforms and rotor wing platforms with aircraft direct control authority. with aircraft direct control authority. Flight Operations are geofence restricting operations to G Direct pilot control authority, semi-autonomous flight modes. airspace with self-limiting capabilities. Flight crew required a maximum of 1. N/A Flight planning software must be able to program multiple GPS Aircraft has the ability to navigate by waypoints at a fixed waypoints with in flight line modifiable options. elevation above the ground based on the terrain. Ability to record sensor data on-board the aircraft. N/A

Payload

Minimum UAS Requirement Target UAS Requirements Configurable payload weight of 1 lb. N/A 13 V1.3 - March 15, 2019 #4 Micro Fixed

Real time video EO payload (day/night) and or IR night vision Real time video EO payload (day/night) and IR night capability (NVG) for nighttime and low light missions with vision capability (NVG) for nighttime and low light ability to record video stream. missions with ability to record video stream. Aircraft is equipped with modular payload design with easily Interface with aircraft IMU/GPS and autopilot (Digital swappable COTS cameras or sensors. interface solution). HD EO/Thermal IR payload with fixed or gimbal mount for mirrorless interchangeable lens camera or RTK capable Gimbal HD EO and Thermal IR video. payload. DSLR, RTK camera mounted to gimbal stabilized N/A mount (option to be fixed at the nadir position). Aircraft autopilot system has the ability to GPS trigger the payload based on GPS location or GPS/IMU distance for N/A appropriate stereo coverage and image overlap at the desired stock payload configuration for photogrammetric stereo imaging. Capable to integrate DGPS/RTK into imagery metadata N/A for high precision mapping missions. Provide MISB (motion imagery standards board) MUXE N/A Video for HD quality or better. The Aircraft IMU telemetry should be embedded into the video metadata.

14 V1.3 - March 15, 2019 #5 T1 Rotor

Flight Performance Minimum UAS Requirement Target UAS Requirements Platform maximum weight under 100 lbs. Platform maximum weight under 35 lbs. Flight duration of 20 minutes with 8lb payload, Flight duration of 45 minutes with 10lb payload, standard day. standard day. N/A Service ceiling 12,000 feet density altitude. Maximum sustained wind speed capability of 20 Maximum sustained wind speed capability of 35 knots. knots. Minimum launch area requirement of 30 feet by 30 Minimum launch area requirement of 10 feet by 10 feet. feet. Minimum recovery area requirement of 30 feet Minimum recovery area requirement of 10 feet by 10 by 30 feet. feet. Vertical take-off and landing (VTOL). N/A Noise level of 60 dB at 100 feet (AGL) at hover N/A with maximum payload. Operating temperature range of 10–110 Operating temperature range of negative 40–110 degrees Fahrenheit. degrees Fahrenheit. N/A Water proof capable. Command and Control Minimum UAS Requirement Target UAS Requirements Communication range (RX/TX) C2 of 1 Miles. Communication range (RX/TX) C2 of 4 to 6 Miles. Transmit video up to 1 Miles. Transmit video range of 4 to 6 Miles. Electric, Gas, or Turbine power supply. Power supply of electric, or non-aviation fuel. N/A Sense and avoid capable Uplink control frequency that is a secure digital data frequency hopping link at 2.4 GHz or 5.8 N/A GHz or 900 MHz ISM Band, WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Downlink frequency that is a secure digital data link at 2.4 GHz and or 5.8 GHz ISM Bands and or 900mhz, N/A w/FIPS compliant WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Loss of Link (LOL) capability: return to launch or Loss of Link (LOL): land at a specified land now. location GPS capable of USA satellite constellations. GPS capable of using all three satellite constellations at the same time: USA (GPS), Russian (GLONASS), and European (Galileo) or superior Selectable LOL: Return to launch, land now, N/A programmable point. Basic manual control along with a GCS (laptop, tablet). Aircraft has the ability to navigate by waypoints at a fixed elevation above the ground based on the terrain. N/A GCS is open source with the ability to be customized. Flight transects are custom generated when user gives a specific area of interest (AOI). The software calculates the optimum flight lines based on sensor height, focal length, width, speed to cover the AOI with specific forward and side lap image %. N/A Ability to geo-fence operations. Flight crew required a maximum of 1, not Flight crew required a maximum of 2. including observer. Aircraft has the ability to navigate by waypoints at a N/A fixed elevation above the ground based on the terrain. 15 V1.3 - March 15, 2019 #5 T1 Rotor

Ability to terminate flight instantaneously. N/A

Payload Specifications Minimum UAS Requirement Target UAS Requirements

Configurable payload weight of 1.5 lbs. Configurable payload weight of 25 lbs. Real time HD EO/IR gimbal payload with video N/A stream that is continuously downloaded and recorded with FPV capability. The ability to mount dual payloads including Gimbaled DSLR HD EO, Thermal IR, or fixed nadir LIDAR Interface with aircraft IMU/GPS and autopilot Aircraft is equipped with modular payload design (Digital interface solution) with easily swappable COTS cameras and camera mounting location. N/A Provide technical specifications for payload interface. Payload interface must provide 5 VDC or 12-14.5 VDC, N/A Serial or USB or Ethernet connections or Micro USB Payload produces geotagged images directly on the SD Payload / log file provides the ability to geotag card. images Capable to integrate DGPS/RTK into imagery metadata N/A for high precision mapping missions. Aircraft Requirements Minimum UAS Requirement Target UAS Requirements A service manual provided. N/A A list of spare parts that would be included in a field N/A service kit and update the list throughout the life of the contract as required. Includes software updates, and updates to N/A latest firmware. Customer Support N/A Data Product and Vendor Specifications Minimum UAS Requirement Target UAS Requirements Flight planning software must be able to program multiple GPS waypoints with the ability to modify N/A flight plans while in flight. Aircraft secured in a hard case capable for transport in N/A a standard SUV and FedEx style shipping. Ability to decline and lock out any device information sharing including telemetry through aircraft, software N/A or applications preventing any automated uploads or downloads Vendor has demonstrated flight experience, list of Vendor currently operating under a COA/Military AWR/FAA current customers with references Cert/NASA Cert. Provide a list of spare parts that would be included in a field service kit. Provide an itemized list of available spare parts and the purchase prices.

16 V1.3 - March 15, 2019 #6 T2 Rotor

Flight Performance Specifications Minimum UAS Requirement Target UAS Requirements Platform maximum weight under 20 lbs. Platform maximum weight under 10 lbs. Flight duration of 30 minutes with max payload, Flight duration of 60 minutes with maximum standard day. payload, standard day. N/A Service ceiling 10,000 feet density altitude. Maximum sustained wind speed capability of 20 Maximum sustained wind speed capability of 35 knots. knots. Minimum launch area requirement of 20 feet by 20 Minimum launch area requirement of 10 feet by 10 feet. feet. Minimum recovery area requirement of 20 feet Minimum recovery area requirement of 10 feet by 10 by 20 feet. feet. Vertical take-off and landing (VTOL). N/A Noise level of 50 dB at 100 feet (AGL) at hover N/A with maximum payload. Operating temperature range of 10–110 Operating temperature range of negative 40–110 degrees Fahrenheit. degrees Fahrenheit. N/A Water proof capable. Command and Control Specifications Minimum UAS Requirement Target UAS Requirements Communication range (RX/TX) C2 of 0.6 Miles. Communication range (RX/TX) C2 of 4 to 6 Miles. Transmit video up to 0.6 Miles. Transmit video range of 4 to 6 Miles. Electric power supply. N/A N/A Sense and avoid capable Uplink control frequency that is a secure digital data frequency hopping link at 2.4 GHz or 5.8 N/A GHz or 900 MHz ISM Band, WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Downlink frequency that is a secure digital data link at 2.4 GHz and or 5.8 GHz ISM Bands and or N/A 900mhz, w/FIPS compliant WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Loss of Link (LOL) capability: return to launch or N/A land now. GPS capable of using USA satellite constellations. GPS capable of using all three satellite constellations at the same time: USA (GPS), Russian (GLONASS), and European (Galileo) or superior Selectable LOL: Return to launch, land now, route N/A retrace, programmable point. Basic manual control Basic manual control along with a GCS (laptop, tablet). N/A GCS is open source with the ability to be customized. N/A Ability to geo-fence operations. Flight crew required a maximum of 1, not Flight crew required a maximum of 1. including observer. Aircraft has the ability to navigate by waypoints at a N/A fixed elevation above the ground based on the terrain. Ability to terminate flight instantaneously.

17 V1.3 - March 15, 2019 #6 T2 Rotor

Payload Specifications Minimum UAS Requirement Target UAS Requirements

Configurable payload weight of 1.5 lbs. Configurable payload weight of 15 lbs. Real time EO video to provide UAS pilot with Real time HD EO/IR gimbal payload with video stream that situational awareness with ability to record on is continuously downloaded and recorded with FPV board. capability. N/A Aircraft is equipped with modular payload design with easily swappable COTS cameras and camera mounting location. N/A Provide technical specifications for payload interface. Payload interface must provide 5 VDC or 12-14.5 VDC, N/A Serial or USB or Ethernet connections or Micro USB Payload produces geotagged images directly on the SD Payload / log file provides the ability to geotag card. images Aircraft Requirements Minimum UAS Requirement Target UAS Requirements A service manual provided. N/A A list of spare parts that would be included in a field N/A service kit and update the list throughout the life of the contract as required. Includes software updates, and updates to N/A latest firmware. Optional Customer Support Customer Support Data Product and Vendor Specifications Minimum UAS Requirement Target UAS Requirements Flight planning software must be able to program multiple GPS waypoints with the ability to modify N/A flight plans while in flight. System secured in backpack sized case capable for N/A commercial carry-on luggage Ability to decline and lock out any device information sharing including telemetry through aircraft, software N/A or applications preventing any automated uploads or downloads System includes a total of 4 Aircraft Batteries System includes a total of 8 Aircraft Batteries

18 V1.3 - March 15, 2019 #7 T3 Rotor

Flight Performance Specifications Minimum Requirements Target Platform maximum weight under 5 lbs. Platform maximum weight under 3 lbs. Flight duration of 20 minutes with max payload, Flight duration of 40 minutes with maximum standard day. payload, standard day. Service ceiling 10,000 feet density altitude. Service ceiling 14,500 feet density altitude. Maximum sustained wind speed capability of 10 Maximum sustained wind speed capability of 30 knots. knots. Minimum launch area requirement of 20 feet by 20 Minimum launch area requirement of 10 feet by 10 feet. feet. Minimum recovery area requirement of 20 feet Minimum recovery area requirement of 10 feet by 10 by 20 feet. feet. Vertical take-off and landing (VTOL). N/A N/A Noise level of 50 dB at 100 feet (AGL) at hover with maximum payload. Operating temperature range of 10–100 Operating temperature range of negative 40–110 degrees Fahrenheit. degrees Fahrenheit. N/A Waterproof capable. Command and Control Specifications Minimum Requirements Target Communication range (RX/TX) C2 of 1 Mile. Communication range (RX/TX) C2 of 3 Miles. Transmit video range of 1 Mile. Transmit video range of 3 Mile. Electric power supply. N/A N/A Obstacle avoidance capable Uplink control frequency that is a secure digital N/A data frequency hopping link at 2.4 GHz or 5.8 GHz or 900 MHz ISM Band, WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Downlink frequency that is a secure digital data link at N/A 2.4 GHz and or 5.8 GHz ISM Bands and or 900mhz, w/FIPS compliant WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Loss of Link (LOL) capability: return to launch or Selectable LOL: Return to launch, land now, land now. programmable point. GPS capable of using USA satellite constellations. GPS capable of using all three satellite constellations at the same time: USA (GPS), Russian (GLONASS), and European (Galileo) or superior Flight controller allows for manual control of the N/A aircraft N/A Ability to geo-fence operations. Flight crew required a maximum of 1, not Flight crew required a maximum of 1. including observer. N/A Aircraft has the ability to navigate by waypoints at a fixed elevation above the ground based on the terrain. Ability to terminate flight instantaneously. N/A

19 V1.3 - March 15, 2019 #7 T3 Rotor

Payload Specifications Minimum Requirements Target

N/A FPV camera, HD video link to provide UAS pilot with situational awareness with ability to record 4K video HD EO stabilized gimbal with ability to record 2K HD EO stabilized gimbal with ability to record 4K video video and 12MP stills onboard. and 20MP stills onboard and configure camera settings via app Gimbal stabilized zoom camera with up to 30x optical N/A and 6x digital zoom with ability to record video and stills onboard and ability to configure camera settings via app FLIR Vue Pro R stabilized gimbal. FLIR Vue Pro R stabilized gimbal with ability to configure camera settings via app Sony RX1R II mapping payload N/A Ricoh GR II mapping payload N/A Micasense rededge M-Multispectral N/A Aircraft is equipped with modular payload design with easily swappable COTS cameras and custom payloads. N/A Provide technical specifications for payload interface. N/A Payload interface must provide 5 VDC or 12-14.5 VDC, Serial or USB or Ethernet connections or Micro USB N/A Payload produces geotagged images directly on the SD card. Miscellaneous Specifications Minimum Requirements Target Autopilot logs are downloadable for georeferencing Autopilot logs are downloadable and images are imagery and troubleshooting automatically geotagged A service manual provided. N/A N/A A list of spare parts that would be included in a field service kit and update the list throughout the life of the contract as required. Includes software updates, and updates to latest N/A firmware. Optional Customer Support Customer Support Flight planning software with free license (available N/A on tablet and laptop Flight planning software for repeatable flights and N/A must display UAS latitude/longitude position and telemetry data System secured in backpack case for field work and System includes backpack and hard case. commercial carry-on luggage Ability to decline and lock out any device information N/A sharing including telemetry through aircraft, software or applications preventing any automated uploads or downloads System includes a total of 4 aircraft batteries equal to System includes a total of 8 aircraft batteries equal to or or less than 100Wh less than 100Wh

20 V1.3 - March 15, 2019 #8 Micro Rotor

Flight Performance Specifications Minimum Requirements Target Platform maximum weight under 2 lbs. Platform maximum weight under 1.7 lbs. Flight duration of 25 minutes with max payload, Flight duration of 40 minutes with maximum standard day. payload, standard day. Service ceiling 10,000 feet density altitude. Service ceiling 15,500 feet density altitude. Maximum sustained wind speed capability of 25 Maximum sustained wind speed capability of 35 knots. knots. Minimum launch area requirement of 10 feet by 10 Minimum launch area requirement of 5 feet by 5 feet. feet. Minimum recovery area requirement of 10 feet Minimum recovery area requirement of 5 feet by 5 by 10 feet. feet. Vertical take-off and landing (VTOL). N/A N/A Noise level of 50 dB at 100 feet (AGL) at hover with maximum payload. Operating temperature range of 10–100 Operating temperature range of negative 40–110 degrees Fahrenheit. degrees Fahrenheit. N/A Waterproof capable. Command and Control Specifications Minimum Requirements Target Communication range (RX/TX) C2 of 3 Mile. Communication range (RX/TX) C2 of 8 Miles. Transmit video range of 3 Mile. Transmit video range of 8 Mile. Electric power supply. N/A N/A Obstacle avoidance capable Uplink control frequency that is a secure digital N/A data frequency hopping link at 2.4 GHz or 5.8 GHz or 900 MHz ISM Band, WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Downlink frequency that is a secure digital data link at N/A 2.4 GHz and or 5.8 GHz ISM Bands and or 900mhz, w/FIPS compliant WPA2 or 128, 192, or 256 bit AES encryption (FIPS compliant). Loss of Link (LOL) capability: return to launch or Selectable LOL: Return to launch, land now, land now. programmable point. GPS capable of using USA satellite constellations. GPS capable of using all three satellite constellations at the same time: USA (GPS), Russian (GLONASS), and European (Galileo) or superior Flight controller allows for manual control of the N/A aircraft Optical stabilization mode N/A Flight crew required a maximum of 1, not Flight crew required a maximum of 1. including observer. Aircraft has the ability to navigate by waypoints at a N/A fixed elevation above the ground based on the terrain. Ability to terminate flight instantaneously. N/A

21 V1.3 - March 15, 2019 #8 Micro Rotor

Payload Specifications Minimum Requirements Target

Ability to live stream HD video for capture 720p FPV camera, HD video link to provide UAS pilot with minimum situational awareness with ability to record 4K video HD EO stabilized gimbal with ability to record 2K HD EO stabilized gimbal with ability to record 4K video video and 12MP stills onboard. and 20MP stills onboard and configure camera settings via app Gimbal stabilized zoom camera with up to 30x optical N/A and 6x digital zoom with ability to record video and stills onboard and ability to configure camera settings via app N/A FLIR stabilized gimbal with ability to configure camera settings via app N/A Ability to do mapping missions from waypoint navigation N/A Provide technical specifications for payload interface. N/A Payload interface must provide 5 VDC or 12-14.5 VDC, Serial or USB or Ethernet connections or Micro USB N/A Payload produces geotagged images directly on the SD card. Miscellaneous Specifications Minimum Requirements Target Autopilot logs are downloadable and images are N/A automatically geotagged A service manual provided. N/A N/A A list of spare parts that would be included in a field service kit and update the list throughout the life of the contract as required. Includes software updates, and updates to latest N/A firmware. Optional Customer Support Customer Support Flight planning software with free license (available N/A on tablet and laptop) Flight planning software for repeatable flights and N/A must display UAS latitude/longitude position and telemetry data System secured in case for field work and commercial System includes backpack and hard case. carry-on luggage Ability to decline and lock out any device information N/A sharing including telemetry through aircraft, software or applications preventing any automated uploads or downloads System includes a total of 6 aircraft batteries equal to System includes a total of 8 aircraft batteries equal to or or less than 100Wh less than 100Wh

22 V1.3 - March 15, 2019 #9 Training Micro Rotor

Flight Performance Specifications Minimum Requirements Target Platform maximum weight 320 grams. N/A Flight duration of 25 minutes with payload, standard Flight duration of 40 minutes with maximum day. payload, standard day. Service ceiling 10,000 feet density altitude. Service ceiling 15,500 feet density altitude. Maximum sustained wind speed capability of 25 Maximum sustained wind speed capability of 35 knots. knots. Vertical take-off and landing (VTOL). N/A Operating temperature range of 14 –104 Operating temperature range of negative 40–110 degrees Fahrenheit. degrees Fahrenheit. N/A Waterproof capable. Command and Control Specifications Minimum Requirements Target Communication range (RX/TX) C2 of 2.5 Mile. Communication range (RX/TX) C2 of 4 Miles. Transmit video range of 2.5 Mile. Transmit video range of 8 Mile. Uplink control frequency that is secure digital N/A data link with FIPS compliant encryption Downlink control frequency that is secure digital data N/A link with FIPS compliant encryption

Loss of Link (LOL) capability: return to launch or Selectable LOL: Return to launch, land now, land now. programmable point. GPS capable of using USA (GPS) satellite GPS capable of using all three satellite constellations at constellations as well as Russian (GOLNASS). the same time: USA (GPS), Russian (GLONASS), and European (Galileo) or superior Flight controller allows for manual control of the N/A aircraft Flight crew required a maximum of 1, not Flight crew required a maximum of 1. including observer. Ability to terminate flight instantaneously. N/A Payload Specifications Minimum Requirements Target Ability to live stream HD video for capture 720p FPV camera, HD video link to provide UAS pilot with minimum situational awareness with ability to record 4K video HD 3 axis stabilized gimbal with ability to record 4K N/A video and capture 21 MP Photos

Gimbal stabilized zoom camera with up to 30x optical N/A and 6x digital zoom with ability to record video and stills onboard and ability to configure camera settings via app N/A FLIR stabilized gimbal with ability to configure camera settings via app N/A Ability to do mapping missions from waypoint navigation

23 V1.3 - March 15, 2019 #9 Training Micro Rotor

Miscellaneous Specifications Minimum Requirements Target Autopilot logs are downloadable and images are N/A automatically geotagged A service manual provided. N/A N/A A list of spare parts that would be included in a field service kit and update the list throughout the life of the contract as required. Includes software updates, and updates to latest N/A firmware. Optional Customer Support Customer Support Flight planning software with free license (available on N/A tablet and laptop) System secured in case for field work and commercial System includes backpack and hard case. carry-on luggage Ability to decline and lock out any device information N/A sharing including telemetry through aircraft, software or applications preventing any automated uploads or downloads System includes a smart battery equal to or less than System includes a total of 6-8 aircraft batteries equal to 100Wh or less than 100Wh

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